A310

SERVICE BULLETIN

SUMMARY

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX FRANCE

Tel : (33) 5 61 93 33 33

Telex : AIRBU 530526F

Fax : (33) 5 61 93 42 51

This summary is for information only and is

not approved for modification of the aircraft

MANDATORY MANDATORY MANDATORY MANDATORY

ATA SYSTEM : 28

TITLE : FUEL - FQI - REPLACE THE COCKPIT MULTI TANK INDICATOR

MODIFICATION No. : 13409H5694

REASON/DESCRIPTION/OPERATIONAL CONSEQUENCES

This Service Bulletin is published to advise all operators of A310 aircraft of the issue of Smiths Vendor

Service Bulletin Nos. 1404KID-28-466 or 1406KID-28-467 or 1410KID-28-468 or 1420KID-28-469.

PCP sleeving has been found to degrade significantly with age and high temperature. This can cause a short

circuit between pins when used on connector back wiring.

This has occurred on the Multi Tank Indicator (MTI) (6QT) used on the flight deck of an A300-600 aircraft. A

similar problem could occur to the MTIs on an A310 aircraft.

This Service Bulletin details instructions to remove and modify the MTI from the cockpit or replace it with

one that has been modified. The modified MTI has white silicone sleeves fitted and will be identified with a

new part number.

Accomplishment of this Service Bulletin will reduce the risk of a short circuit between pins of the MTI (6QT).

EVALUATION TABLE

COMPLIANCE Mandatory CANCELS INSPECTION SB No

POTENTIAL AD Yes A/C OPERATION AFFECTED No

RELIABILITY AFFECTED No PAX COMFORT AFFECTED No

COST SAVING No ETOPS AFFECTED No

DATE : Jun 04/08 SERVICE BULLETIN No. : A310-28-2167

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A310

SERVICE BULLETIN

SUMMARY

EVALUATION TABLE

STRUCTURAL LIFE EXTN No VENDOR SB INVOLVED Yes

KIT PRICE (USD) See SB

MODIFICATION CLASSIFICATION

MAJOR 13409H5694

MINOR None

As per EASA IR 21, a minor change is one that has no appreciable effect on the mass, balance, structural

strength, reliability, operational characteristics affecting the airworthiness of the product. All other changes

are major changes.

EFFECTIVITY

This Service Bulletin is applicable to this (these) operator(s) :

34W 58X 82Z 99Y A1L AIC ARG BAF BBC BLM CFC CSA DAH DGA F2I FDX GAF IRA IRM IYE JAB

JAV KAC KTC MGL MPD MPJ MWA PIA QAF QSC R1T RJA ROT RZO SBI SGX SUD TAP THY TSC

UAE UZB WHT

NOTE : Accomplishment of this modification is by Service Bulletin only.

CONCURRENT REQUIREMENTS

None

REFERENCES/REPERCUSSIONS

TFU : 28.40.00.01

OEB : None

AOT : None

SIL : None

LIFE LIMIT : None

LINE MAINTENANCE AFFECTED : No

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A310

SERVICE BULLETIN

SUMMARY

OTHERS : None

NATURE OF THE WORK

AIRCRAFT : Yes

EQUIPMENT : Yes

HARD : No

SOFT : No

OBRM : No

MANPOWER

Config. 01

TOTAL MANHOURS 1.5*

ELAPSED TIME (HOURS) 1.5*

NOTE(*) Refer to Smiths VSB No. 1404KID-28-466 or 1406KID-28-467 or 1410KID-28-468 or

1420KID-28-469 for the modification manhours.

MATERIAL INFORMATION

AIRCRAFT DATA

Refer to Smiths Vendor Service Bulletin Nos. 1404KID-28-466 or 1406KID-28-467 or 1410KID-28-468

or 1420KID-28-469.

APPENDICES

None

DATE : Jun 04/08 SERVICE BULLETIN No. : A310-28-2167

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A310

SERVICE BULLETIN

This Page Intentionally Left Blank

DATE : Jun 04/08 SERVICE BULLETIN No. : A310-28-2167

REVISION No. : 00 - Page : 4

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A310

SERVICE BULLETIN

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX FRANCE

Tel : (33) 5 61 93 33 33

Telex : AIRBU 530526F

Fax : (33) 5 61 93 42 51

MANDATORY MANDATORY MANDATORY MANDATORY

ATA SYSTEM : 28

TITLE : FUEL - FQI - REPLACE THE COCKPIT MULTI TANK INDICATOR

MODIFICATION No. : 13409H5694

This document contains AIRBUS PROPRIETARY INFORMATION and shall at all times remain the property

of AIRBUS; no intellectual property right or licence is granted by AIRBUS in connection with any information

contained in it. It is delivered on the express condition that said document and the information contained in

it shall be treated as confidential, shall not be used for any purpose other than that for which it is hereby

delivered. It shall not be disclosed in whole or in part to third parties and shall not be duplicated in any

manner (except for the purposes of performing the tasks described hereunder and provided that any recipient

of such document shall comply with the conditions herein), without AIRBUS’ prior written consent.

1. PLANNING INFORMATION

A. EFFECTIVITY

(1) Models

310-203 310-203C 310-204 310-221 310-222 310-304 310-308 310-322 310-324 310-325

(2) Aircraft

(a) Effectivity by MSN

This Service Bulletin is applicable to aircraft MSN:

0162 0191 0201 0217 0224 0230 0233 0237 0241 0245 0248 0251 0254 0257 0260

0264 0267 0273 0278 0281 0283 0288 0291 0293 0297 0303 0309 0313 0316 0318

0320 0326 0331 0333 0335 0338 0339 0342 0343 0345 0346 0349 0353 0355-0357

0359 0360 0362 0364 0367 0369 0370 0372 0375 0378 0379 0386 0389 0390 0392

0394 0397 0399 0400 0406 0407 0410 0413 0416 0418 0419 0421 0422 0425

0427-0431 0434 0436 0437 0439 0441 0444-0449 0451-0458 0467 0468 0472 0473

0475 0476 0478 0480-0492 0494-0500 0502 0503 0519 0520 0522-0524 0526 0527

0531 0534 0535 0537-0539 0541 0542 0544 0545 0547-0552 0562 0564 0565 0567

0568 0571 0573 0574 0576 0585-0595 0597-0600 0620 0622 0624 0634 0636

0638 0640 0642 0644 0646-0654 0656 0658 0660 0661 0663 0665 0667 0669

0671 0672 0674 0676 0678 0680 0682 0684 0686 0687 0689 0691 0693 0695

0697 0700 0702 0704 0706

(b) Effectivity by Operator

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A310

SERVICE BULLETIN

The Operator/MSN relationship is provided for information only and is correct at the

time of issue in accordance with the information available to AIRBUS. Any future

changes resulting from transfer of an aircraft from one operator to another will not be

reflected in this list unless the Service Bulletin is revised for another reason.

OPERATOR MSN

34W 0399

58X 0431

82Z 0550 0551

99Y 0489

A1L 0648

AIC 0392 0406 0407 0413 0428 0429 0538 0544 0598 0654 0665 0669

0680 0684 0693 0695 0697

ARG 0640 0686

BAF 0367 0372

BBC 0594 0650 0700

BLM 0488

CFC 0425 0441 0444 0446 0482

CSA 0564 0567 0672 0674

DAH 0291 0293

DGA 0418 0421 0422

F2I 0309

FDX 0162 0191 0201 0217 0224 0230 0233 0237 0241 0245 0248 0251

0254 0257 0260 0264 0267 0273 0278 0281 0283 0288 0297 0303

0313 0316 0318 0326 0331 0333 0335 0339 0342 0343 0345 0346

0349 0353 0355 0356 0359 0360 0362 0364 0369 0378 0394 0397

0400 0439 0449 0452 0454 0456 0457 0458 0467 0492 0500 0534

0539 0542 0549 0552 0589 0593 0634 0638

GAF 0434 0484 0498 0499 0503 0522 0523

IRA 0338 0370 0375 0379 0389 0390 0436 0671

IRM 0537 0586

IYE 0535 0568 0702 0704

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A310

SERVICE BULLETIN

OPERATOR MSN

JAB 0320 0419

JAV 0357 0481

KAC 0647 0649 0663

KTC 0524

MGL 0526

MPD 0451 0453 0455 0642

MPJ 0410

MWA 0652

PIA 0473 0585 0587 0590 0653 0656 0660 0676 0678 0682 0687

0689 0691

QAF 0667

QSC 0620

R1T 0591

RJA 0416 0445 0490 0491 0531

ROT 0636 0644

RZO 0571 0624 0651 0661

SBI 0427 0430 0468 0475 0486 0487 0520

SGX 0519 0562

SUD 0437 0548

TAP 0483 0494 0495 0541 0565

THY 0386 0476 0478 0480 0496 0497 0502

TSC 0447 0472 0485 0527 0545 0547 0588 0595 0597 0599 0600 0658

UAE 0592 0622 0646

UZB 0574 0576 0706

WHT 0448 0573

(c) Effectivity by MSN and Kit/Configuration

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A310

SERVICE BULLETIN

The Kits and configurations applicable to these MSNs are given at the end of this list

0162 0191 0201 0217 0224 0230 0233 0237 0241 0245 0248 0251 0254 0257 0260

0264 0267 0273 0278 0281 0283 0288 0291 0293 0297 0303 0309 0313 0316 0318

0320 0326 0331 0333 0335 0338-0339 0342-0343 0345-0346 0349 0353 0355-0357

0359-0360 0362 0364 0367 0369-0370 0372 0375 0378-0379 0386 0389-0390 0392

0394 0397 0399-0400 0406-0407 0410 0413 0416 0418-0419 0421-0422 0425

0427-0431 0434 0436-0437 0439 0441 0444-0449 0451-0458 0467-0468 0472-0473

0475-0476 0478 0480-0492 0494-0500 0502-0503 0519-0520 0522-0524

0526-0527 0531 0534-0535 0537-0539 0541-0542 0544-0545 0547-0552 0562

0564-0565 0567-0568 0571 0573-0574 0576 0585-0595 0597-0600 0620 0622

0624 0634 0636 0638 0640 0642 0644 0646-0654 0656 0658 0660-0661 0663 0665

0667 0669 0671-0672 0674 0676 0678 0680 0682 0684 0686-0687 0689 0691

0693 0695 0697 0700 0702 0704 0706

KIT No. QTY PER A/C CONFIGURATION

None 01

NOTE : Config. 01 is valid for all the aircraft given in the effectivity of this Service

Bulletin as a standard configuration.

(3) Spares

Refer to Smiths VSB Nos. 1404KID-28-466 or 1406KID-28-467 or 1410KID-28-468 or

1420KID-28-469.

B. CONCURRENT REQUIREMENTS

None

C. REASON

(1) History

PCP sleeving has been found to degrade significantly with age and high temperature. This

can cause a short circuit between pins when used on connector back wiring.

This has occurred on the MTI (6QT) used on the flight deck of an A300-600 aircraft. A

similar problem could occur to the MTIs on an A310 aircraft.

(2) Objective/Action

This Service Bulletin details instructions to remove and modify the MTI from the cockpit or

replace it with one that has been modified. The modified MTI has white silicone sleeves

fitted and will be identified with a new part number.

This Service Bulletin is published to advise all operators of A310 aircraft of the issue

of Smiths Vendor Service Bulletin Nos. 1404KID-28-466 or 1406KID-28-467 or

1410KID-28-468 or 1420KID-28-469.

(3) Advantages

DATE : Jun 04/08 SERVICE BULLETIN No. : A310-28-2167

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A310

SERVICE BULLETIN

Accomplishment of this Service Bulletin will reduce the risk of a short circuit between

pins of the MTI (6QT).

(4) Operational/Maintenance Consequences

None

D. DESCRIPTION

To accomplish this Service Bulletin it is necessary to :

(1) Config. 01

(a) Remove the MTI (6QT) from the cockpit panel 20VU.

(b) Do the Smiths VSB Nos. 1404KID-28-466 or 1406KID-28-467 or 1410KID-28-468

or 1420KID-28-469 or replace it with a modified MTI.

(c) Install the modified MTI (6QT) to the cockpit panel 20VU.

E. COMPLIANCE

(1) Classification

Mandatory

(2) Accomplishment Timescale

Accomplishment of this Service Bulletin has been rendered mandatory by the issue of an

Airworthiness Directive (AD) published by the European Aviation Safety Agency (EASA).

The AD must be used as the reference document for the mandatory accomplishment

timescale.

F. APPROVAL

Approved under EASA Design Organisation Approval No. EASA.21J.031.

If an aircraft listed in the effectivity has a modification or repair embodied that is not of AIRBUS

origin, and which affects the content of this Service Bulletin, the operator is responsible for

obtaining approval by its airworthiness authority for any adaptation necessary before incorporation

of the Service Bulletin.

G. MANPOWER

The manpower estimates given in this Service Bulletin are based on the direct labor cost to do the

work. These estimates assume that the work will be done by experienced personnel, and may

need to be revised upwards to suit operator’s circumstances. The estimates do not include the

time to prepare, plan or inspect the work. Manufacture and procurement of parts and tools, drying

times for paints, sealants, etc, and general administration work are also not included.

Config. 01

Get Access 0.5

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A310

SERVICE BULLETIN

Modification *

Test 0.5

Close up 0.5

TOTAL MANHOURS 1.5

ELAPSED TIME (HOURS) 1.5

NOTE(*) Refer to Smiths VSB No. 1404KID-28-466 or 1406KID-28-467 or 1410KID-28-468 or

1420KID-28-469 for the modification manhours.

H. WEIGHT AND BALANCE

Not changed

I. ELECTRICAL LOAD DATA

Not changed

J. REFERENCES

Aircraft Maintenance Manual (AMM) : 28-42-00 28-42-41

Elec. Std. Practices Manual (ESPM) : 20-55-00

Smiths Vendor Service Bulletin 1404KID-28-466

Smiths Vendor Service Bulletin 1406KID-28-467

Smiths Vendor Service Bulletin 1410KID-28-468

Smiths Vendor Service Bulletin 1420KID-28-469

K. PUBLICATIONS AFFECTED

None

L. INTERCHANGEABILITY/MIXABILITY

DESCRIPTION OLD PART No. NEW PART No. INT MIXABILITY

MTI 1404KID-2 1404KID52 01 No

MTI 1405KID-2 1405KID52 01 No

MTI 1406KID-03 1406KID53 01 No

MTI 1408KID-01-002 1408KID51 01 No

MTI 1409KID-02 1409KID52 01 No

MTI 1410KID-01 1410KID51 01 No

MTI 1411KID-01 1411KID51 01 No

MTI 1414KID-01 1414KID51 01 No

MTI 1415KID-01 1415KID51 01 No

MTI 1420KID1-1 1420KID51-1 01 No

DATE : Jun 04/08 SERVICE BULLETIN No. : A310-28-2167

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A310

SERVICE BULLETIN

DESCRIPTION OLD PART No. NEW PART No. INT MIXABILITY

MTI 1421KID1-1 1421KID51-1 01 No

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SERVICE BULLETIN

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SERVICE BULLETIN

2. MATERIAL INFORMATION

A. MATERIAL - PRICE AND AVAILABILITY

(1) Material

Modification of removed equipment should be negotiated directly with Smiths as per

instructions given in VSB Nos. 1404KID-28-466 or 1406KID-28-467 or 1410KID-28-468 or

1420KID-28-469.

(2) Price and Availability

Refer to Smiths VSB Nos. 1404KID-28-466 or 1406KID-28-467 or 1410KID-28-468 or

1420KID-28-469 for the equipment modification sales terms.

B. INDUSTRY SUPPORT INFORMATION

Refer to Smiths VSB Nos. 1404KID-28-466 or 1406KID-28-467 or 1410KID-28-468 or

1420KID-28-469 for the industry support terms.

C. LIST OF COMPONENTS

Refer to Smiths VSB Nos. 1404KID-28-466 or 1406KID-28-467 or 1410KID-28-468 or

1420KID-28-469.

D. LIST OF MATERIALS - OPERATOR SUPPLIED

(1) Consumable Materials

To accomplish this Service Bulletin it will be necessary to use the consumable materials

listed in Smiths VSB Nos. 1404KID-28-466 or 1406KID-28-467 or 1410KID-28-468 or

1420KID-28-469.

(2) Components

To accomplish this Service Bulletin it will be necessary to use the expendable parts

listed in Smiths VSB Nos. 1404KID-28-466 or 1406KID-28-467 or 1410KID-28-468 or

1420KID-28-469.

E. PARTS TO BE RE-IDENTIFIED BY THE OPERATOR

Refer to Smiths VSB Nos. 1404KID-28-466 for the parts that follow:

ITEM NEW PART No. KEYWORD ITEM OLD PART No. INT

1404KID52 MTI 1404KID-2 01

1405KID52 MTI 1405KID-2 01

Refer to Smiths VSB Nos. 1406KID-28-467 for the parts that follow:

ITEM NEW PART No. KEYWORD ITEM OLD PART No. INT

1406KID53 MTI 1406KID-03 01

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SERVICE BULLETIN

ITEM NEW PART No. KEYWORD ITEM OLD PART No. INT

1408KID51 MTI 1408KID-01-002 01

1409KID52 MTI 1409KID-02 01

Refer to Smiths VSB Nos. 1410KID-28-468 for the parts that follow:

ITEM NEW PART No. KEYWORD ITEM OLD PART No. INT

1410KID51 MTI 1410KID-01 01

1411KID51 MTI 1411KID-01 01

1414KID51 MTI 1414KID-01 01

1415KID51 MTI 1415KID-01 01

Refer to Smiths VSB Nos. 1420KID-28-469 for the parts that follow:

ITEM NEW PART No. KEYWORD ITEM OLD PART No. INT

1420KID51-1 MTI 1420KID1-1 01

1421KID51-1 MTI 1421KID1-1 01

F. TOOLING - PRICE AND AVAILABILITY

None

G. SPECIAL TOOLS

None

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A310

SERVICE BULLETIN

3. ACCOMPLISHMENT INSTRUCTIONS

A. GENERAL

WARNING : MAKE SURE THAT YOU OBEY ALL THE WARNINGS AND ALL THE CAUTIONS

INCLUDED IN THE REFERENCED PROCEDURES.

CAUTION : ALWAYS OBEY THE PRECAUTIONS THAT FOLLOW TO KEEP ELECTRICAL

WIRING IN A SATISFACTORY CONDITION (ELECTRICALLY AND MECHANICALLY

SERVICEABLE). WHEN YOU DO MAINTENANCE WORK, REPAIRS OR

MODIFICATIONS, ALWAYS KEEP ELECTRICAL WIRING, COMPONENTS AND

THE WORK AREA AS CLEAN AS POSSIBLE. TO DO THIS:

- PUT PROTECTION, SUCH AS PLASTIC SHEETING, CLOTHS, ETC; AS

NECESSARY ON WIRING AND COMPONENTS.

- REGULARLY REMOVE ALL SHAVINGS, UNWANTED MATERIAL AND OTHER

CONTAMINATION.

THESE PRECAUTIONS WILL DECREASE THE RISK OF CONTAMINATION AND

DAMAGE TO THE ELECTRICAL WIRING INSTALLATION.

IN CASE OF CONTAMINATION REFER TO ESPM 20-55-00, CLEANING.

(1) Preparation

(a) Config. 01

1 Do the job set up procedure for the removal of the MTI (6QT) from the cockpit

(Refer to AMM 28-42-41, Page block 401).

(2) Standard Practices

(a) Put blanking caps on all the related disconnected electrical-connectors.

B. MODIFICATION

(1) Config. 01

(a) Remove the MTI (6QT) from the cockpit panel 20VU (Refer to AMM 28-42-41,

Page block 401).

(b) Do the Smiths VSB Nos. 1404KID-28-466 or 1406KID-28-467 or 1410KID-28-468

or 1420KID-28-469.

(c) Install the modified MTI (6QT) to the cockpit panel 20VU (Refer to AMM 28-42-41,

Page block 401).

C. TEST

(1) Config. 01

(a) Do the operational test of the MTI (6QT) (Refer to AMM 28-42-00, Page block 501).

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A310

SERVICE BULLETIN

D. CLOSE UP

(1) Config. 01

(a) Do the close up procedure for the installation of the MTI (6QT) Refer to AMM

28-42-41, Page block 401).

(b) Make sure that the work areas are clean and clear of tools and other items of

equipment.

E. DOCUMENTATION

Write in the applicable aircraft records that you have done all the work given in the Service Bulletin.

DATE : Jun 04/08 SERVICE BULLETIN No. : A310-28-2167

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SERVICE BULLETIN

REPORTING SHEET

TITLE : FUEL - FQI - REPLACE THE COCKPIT MULTI TANK INDICATOR

MODIFICATION No. : 13409H5694

Please complete the appropriate item (A or B):

A - SB WILL BE embodied .................................................................. YES/NO (if NO please comment)

If YES, aircraft concerned (as per SB effectivity by default) and planned dates (month/year) of embodiement:

.............................................................................................................................................................................

.............................................................................................................................................................................

B - SB HAS BEEN embodied on aircraft: ............................................................................................................

.............................................................................................................................................................................

.............................................................................................................................................................................

Operator comments:............................................................................................................................................

.............................................................................................................................................................................

.............................................................................................................................................................................

From Airline: ........................................................................................................................................................

Name/Title: ..........................................................................................................................................................

Signature:..................... Date: .....................................................

If operational documentation is affected (see Paragraph 1.K of this SB): If information is needed prior to next

normal revision or prior to SB embodiment, please indicate required service(s):

Either : Advance data................................................................................... YES/NO

Or : Intermediate/Temporary revision ..................................................... YES/NO

Important Information: This SB will only be incorporated in your maintenance and operational documentation

if this sheet is returned to Airbus and signed by a duly authorised representative. With the next feasible

revision, this will result in

- updating of maintenance documentation to show pre and post SB data.

- updating of maintenance and operational documentation to show post SB data

after embodiment.

If this SB requires previous or simultaneous accomplishment of other SBs, Airbus shall automatically include

them in the manual revisions. Refer to SIL 00-037 for detailed information.

Please return this completed sheet to:

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX FRANCE

Attn: SEDCC1 Technical Data and Documentation Services

FAX: (+33) 5 61 93 28 06

e-mail: sb.reporting@airbus.com

Or via your Resident Customer Support Office.

Alternatively, SB lists via letters or fax are also accepted.

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SERVICE BULLETIN

REPORTING QUALITY

TITLE : FUEL - FQI - REPLACE THE COCKPIT MULTI TANK INDICATOR

MODIFICATION No. : 13409H5694

Use this form to tell us what is your perception of the quality of this Service Bulletin.The reported data that you

provide us will be used to analyse areas of difficulties and to take corrective action to futher improve the quality

of our Service Bulletins.

We thank you for the time you have taken in completing this form.

(Please rate on a scale of 1 to 4, with 4 being the highest score)

-Quality rating of this SB 4 3 2 1

-Quality rating of the Accomplishment Instructions 4 3 2 1

-Quality rating of the Illustrations 4 3 2 1

-Is this SB easy to understand ? Y / N

If you have had difficulties in the accomplishment of this SB please quote below the area(s) and give a short

description of the issue.

Planning Material Instructions

X Effectivity X Kit Content X Preparation

X Reason X List of Materials X Mod/Inspection

X Manpower Operator Supplied X Test

X References X Re-identification X Close-up

X Publication X Tooling X Illustrations

Comments :

Operator : Date:

Name/Title :

Please return this form to:

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX FRANCE

Attn: SEMB Service Bulletins Management

FAX: (+33) 5 61 93 42 51

Or via your Resident Customer Support Office.

DATE : Jun 04/08 SERVICE BULLETIN No. : A310-28-2167

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